View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 43131U 18004W 22175.71214936 .00014809 00000-0 41635-3 0 9999
2 43131 97.3759 255.0076 0004595 328.6356 31.4614 15.36595470247697
| Epoch (UTC): | 24 June 2022 17:05:29 |
| Eccentricity: | 0.0004595 |
| inclination: | 97.3759° |
| perigee height: | 453 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 255.0076° |
| argument of perigee: | 328.6356° |
| revolutions per day: | 15.36595470 |
| mean anomaly at epoch: | 31.4614° |
| orbit number at epoch: | 24769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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